• DocumentCode
    1704092
  • Title

    Failure propagation analysis of aircraft engine system based on the small-world net model

  • Author

    Liu Xiaofeng ; An Siqi

  • Author_Institution
    Sch. of Transp. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2013
  • Firstpage
    1214
  • Lastpage
    1219
  • Abstract
    To find the failure propagation mechanism from the complex electromechanical system of aircraft engine, this paper used the topological structure to describe the coupling relations, discussing the role of topological geometry method in the failure propagation. The topological structure statistical properties of the system were analyzed with small world net theory??and a failure propagation model based on the small world clustering was proposed, and the failure propagation paths and relevant key nodes with high pervasion ability were found with the Dijkstra algorithm. The results verify that this method can effectively find the weak point in the system, and provide an important basis for design improvements and failure prevention.
  • Keywords
    electromechanical actuators; engines; failure analysis; parallel algorithms; pattern clustering; Dijkstra algorithm; aircraft engine system; design improvements; electromechanical system; failure prevention; failure propagation analysis; small world clustering; small-world net model; topological geometry method; topological structure; Aircraft propulsion; Analytical models; Atmospheric modeling; Educational institutions; Electronic mail; Pain; Principal component analysis; Aircraft Engine System; Highest Risk Path of Failure Propagation; Intensity of Failure Propagation; Parameter of Network Topological Structure; Small-World Net Model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6639612